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METRO III - ICAO ANNEX 8 FAAAPPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR METRO III, SA227-AC ICAO ANNEX ‘8 - 14,500 POUNDS TAKEOFF WITH SRL OFF/INOPERATIVE Registration No. Serial No. This supplement must be attached to operations are conducted with either, information contained in this document listed. For limitations, procedures, and the basic Airplane Flight Manual.

the FAA Approved Airplane Flight Manual when takeoff and flight or both, of the Single Red Line (SRL) systems inoperative. The supplements or supersedes the basic manual only in those areas performance information not contained in this supplement, consult

FAA Approved by: A Michele M. Owsley Manager, Aircraft Certification Office Federal Aviation Administration Ft. Worth, Texas 76193-0150

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

Supplement B-l Page 1 of 12 4AC

METRO III – ICAO ANNEX 8 LIST OF REVISIONS Revisions to the Airplane Flight Manual provide current information applicable to operation of the SA227-AC aircraft. Revised pages should be inserted in the manual to replace existing pages or to add additional pages, as applicable. The manual is valid only when all current revisions are incorporated.

Revision Number N/A

Revised Pages All

FAA Approved Description of Revision

Signature

Supplement renumbered and reprinted to complement AFM Reissue B. Replaces former Supplement A-2.

Date

See Page 1

A black bar in the margin of a revised page shows the current change.

Supplement B-1 Page 2 of 12 4AC

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

METRO III – ICAO ANNEX 8 INTRODUCTION This supplement presents information relative to operation of the Garrett TPE331-11U-601G or -611G engine with the Single Red Line (SRL) system inoperative. The performance contained in the basic flight manual is applicable. However, limiting takeoff and landing performance is determined by entering the charts at actual outside air temperature (OAT) plus 5oC whenever expected torque is less than 100%, that is, when power is limited by ambient conditions. In that case, takeoff torque is set using care to avoid exceeding maximum allowed SRL INOP EGT. Maximum EGT will vary with the OAT. The placard shown in this supplement must be installed prior to takeoff operations with an SRL system inoperative.

SECTION 1 . . . . . . .LIMITATIONS

ENGINE OPERATION WITH CONTINUOUS ALCOHOL WATER INJECTION (CAWI) Takeoff with CAWI is prohibited when either SRL system is inoperative.

SINGLE RED LINE COMPUTER (SRL) Takeoff operations with either or both SRL systems inoperative is permitted when the airplane is operated in accordance with this supplement and in accordance with an approved MEL. That MEL must refer to this supplement for takeoff and continued flight operations with SRL system(s) inoperative.

For SRL inoperative operations, takeoff with BOTH cabin bleed air and engine anti-ice ON is prohibited.

(Either one may be used during takeoff, provided the other one is OFF).

OPERATING WEIGHTS Whenever the expected torque, determined from entering the Takeoff Power Check Charts at actual pressure altitude and actual OAT plus 5oC, is less than 100%, the maximum operating weights listed in the LIMITATIONS section of the basic flight manual or applicable supplement, must be determined by entering the appropriate performance charts with the actual outside air temperature plus 5oC.

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

Supplement B-1 Page 3 of 12 4AC

METRO III – ICAO ANNEX 8 SECTION 1 . . . . . . .LIMITATIONS (continued) PLACARDS To be installed aft of the compass fairing for operations with SRL system(s) inoperative.

SRL INOP EGT LIMITS FOR DRY POWER TAKEOFF OR GO - AROUND AT 100% RPM : OAT EGT (oC) (oF) (oC) 50 40 30 20 10 0 –10 –20 –30 –40

122 104 86 68 50 32 14 –4 –22 –40

614 603 593 583 574 566 559 553 549 545

WHEN EGT LIMITED, ENTER AFM PERFORMANCE CHARTS AT OAT +5oC

FOR MCP AT V YSE :

IOAT (oC)

EGT (oC)

50 40 30 20 10 0 –10 –20 –30 –40

620 609 599 589 580 572 566 560 555 551

SECTION 2 . . . . . . .NORMAL PROCEDURES This supplement does not change normal procedures of the basic AFM. Section 3A of this supplement provides abnormal procedures to be followed when an SRL system has been found inoperative.

Supplement B-1 Page 4 of 12 4AC

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

METRO III – ICAO ANNEX 8 SECTION 3 . . . . . . .EMERGENCY PROCEDURES In any takeoff or go-around situation requiring takeoff power when both SRL systems are inoperative, set the placarded SRL INOP LIMIT EGT for the existing OAT or 100% torque, whichever is encountered first.

In any climb situation requiring maximum continuous power (MCP) when both SRL systems are inoperative, set the EGT value from Figure 3A-1 in the basic manual or 100% torque, whichever is encountered first. The bottom table of the cockpit placard on page 4 of this supplement is extracted from Figure 3A-1 and provides limit EGT for setting MCP when flying at single engine best rate of climb speeds.

If only one SRL system is inoperative, proper power setting of the engine with the inoperative SRL can be obtained by matching the torque of the engine with the inoperative SRL to that of the engine with the operative SRL. It is important to monitor engine indications to ensure that SRL INOP LIMIT EGT is not exceeded.

CAUTION TEMPERATURE LIMITER PROTECTION IS NOT AVAILABLE WHEN THE SRL SYSTEM IS INOPERATIVE. SET POWER LEVERS CAREFULLY WHEN ABOVE 50% POWER TO ALLOW FOR EGT INDICATION LAG. IMPROPER POWER MANAGEMENT CAN RESULT IN ENGINE OVER TEMPERATURE CONDITIONS.

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

Supplement B-1 Page 5 of 12 4AC

METRO III – ICAO ANNEX 8 SECTION 3A . . . . . . .ABNORMAL PROCEDURES FLIGHT OPERATIONS WITH SRL SYSTEM(S) INOPERATIVE PREFLIGHT Use procedure in Section 2, basic manual.

BEFORE STARTING ENGINES Use procedure in Section 2, basic manual with following exceptions: •

SRL – ∆ P/P Power Switch (affected engine) ....................................................................... SRL OFF

•

Temperature Limiter Circuit Breaker (affected engine) ............................................................... PULL

•

Use actual OAT + 5oC to determine maximum allowable takeoff weight and the takeoff torque to be used on both engines.

•

Use actual OAT to determine the maximum allowable SRL INOP EGT on the engine(s) with inoperative SRL for takeoff and initial climb or go-around operations from Figure 1 or the cockpit placard.

MAXIMUM ALLOWABLE EGT WITH SRL OFF / INOPERATIVE DRY POWER AT 100% RPM, 0 TO 150 KIAS 620

LIMIT EGT ( C)

600

580

560

NOTE IOAT NOTED WHEN PARKED OR TAXIING MAY NOT BE ACCURATE.

540 -40

-40

-20

-30

0

-20

20

-10

40

0

60

10

80

20

100

30

120

40

50

( F)

( C)

OUTSIDE AIR TEMPERATURE

FIGURE 1 Supplement B-1 Page 6 of 12 4AC

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

METRO III – ICAO ANNEX 8 SECTION 3A . . . . . . .ABNORMAL PROCEDURES (continued) BATTERY OR GPU START Use appropriate Manual Ground Start Procedure in Section 3A, basic manual. The note on page 3A-9 (which is repeated at step 21, page 3A-11, and at step 22, page 3A-14) is not applicable when operating in accordance with this supplement.

BEFORE TAXI Use procedure in Section 2, basic manual. Omit step 14, Single Red Line Computer / Temp Limiter Check, which is not applicable when operating in accordance with this supplement.

TAXI Use procedure in Section 2, basic manual.

BEFORE TAKEOFF Use procedure in Section 2, basic manual.

TAKEOFF – (DRY) (Use of CAWI is not authorized) *1. Bleed Air Switches ................................................................................................... AS DESIRED NOTE Takeoff with both bleed air on and engine anti-ice on is not authorized when either SRL system is inoperative. *2. Speed Levers ............................................................................................... HIGH RPM/SRL OFF ANNUNCIATOR LIGHTS ON / FRICTION SET WARNING IF FLIGHT IS ATTEMPTED WITH THE SPEED LEVERS SET AT LOW RPM, DIVERGENT POWER OSCILLATIONS ARE LIKELY TO OCCUR IF THE TEMPERATURE LIMITING RANGE IS REACHED. SUCH POWER OSCILLATIONS MUST BE AVOIDED

BY ENSURING THAT THE SPEED LEVERS ARE SET TO OBTAIN PROPER ENGINE SPEED. See Note on next page

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

Supplement B-1 Page 7 of 12 4AC

METRO III – ICAO ANNEX 8 SECTION 3A . . . . . . .ABNORMAL PROCEDURES (continued) TAKEOFF – (DRY) (Use of CAWI is not authorized) (continued) NOTE Both SRL OFF lights will be illuminated if both SRL systems are inoperative. The SRL OFF light for an engine with operative SRL system should go out when RPM increases beyond 80%.

3. Engine Speed .................................................................................. CHECK 96% TO 97.5% RPM 4. Ignition Mode Switches ......................................................................................... AS REQUIRED OR Auto/Cont Ignition Switches ................................................................................ AUTO OR CONT 5. Power Levers ......................................................................................... SET TAKEOFF POWER. DO NOT EXCEED LIMIT EGT OR 97% TORQUE CAUTION • TEMPERATURE LIMITER PROTECTION IS NOT AVAILABLE WHEN THE SRL SYSTEM IS INOPERATIVE. IMPROPER POWER MANAGEMENT CAN RESULT IN ENGINE OVER TEMPERATURE CONDITIONS. • DO NOT ALLOW TORQUE TO EXCEED 100% DURING TAKEOFF. 6. Engine Speed ................................................................................. CHECK 100% TO 101% RPM CAUTION IF RPM IS ALLOWED TO DECREASE TO BELOW 99% WITH THE TEMPERATURE LIMITING SYSTEM OPERATING, ENGINE POWER SURGES MAY OCCUR WHEN THE SRL COMPUTER TRANSITIONS BACK AND FORTH BETWEEN ITS SPEED/ TEMPERATURE SCHEDULES. 7. Brakes ............................................................................................................................RELEASE 8. NWS Power Lever Button ........................................................................................ AS DESIRED NOTE • Normal authority steering is available until deactivated by landing gear squat switches at liftoff unless modified.

• On those aircraft which have been modified in accordance with Service Bulletin 32-006, normal authority steering is available until deactivated by landing gear retraction.

9. V1 Speed..........................................................................................................................ROTATE 10. Landing Gear (after liftoff) ......................................................................................................... UP 11. Flaps (above 115 KIAS) ............................................................................................................ UP Supplement B-1 Page 8 of 12 4AC

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

METRO III – ICAO ANNEX 8 SECTION 3A . . . . . . .ABNORMAL PROCEDURES (continued) CLIMB 1. Climb Speed ...................................................................................................................... ATTAIN 2. Bleed Air Switches ................................................................................................... AS DESIRED 3. Climb Power .................................................. NOT TO EXCEED LIMIT EGT OR 100% TORQUE NOTE • Reduce EGT 50°C or more before reducing RPM of engine(s) operating with SRL system inoperative. Set RPM to 97% or 100%.

Advance power lever to desired EGT that does not exceed limit EGT per Section 3A of basic manual.

• It is permissible to continue two engine climbs with takeoff power SRL INOP EGT set. However, additional performance is available by advancing power to MCP. MCP, as shown in Section 3A or the cockpit placard, must be used to obtain single engine best rate of climb. *4.

5.

6. *7.

8.

9.

Propeller Synchrophaser Switch (if installed) .................................................... CLIMB & CRUISE Ice Protection Systems ......................................................................................... AS REQUIRED Cabin Pressure Scheduling ................................................................................................ CHECK No Smoking – Fasten Seat Belt Signs .................................................................. AS REQUIRED Nose Wheel Steering Switch ................................................................................................... OFF Ignition Mode Switches ................................................................... NORMAL OR AS REQUIRED OR Auto/Cont Ignition Switches ................................................................................ AUTO OR CONT

10,000 FEET ......................................................................................................... CHECK AS FOLLOWS 1. Ammeters ...........................................................................................................................CHECK 2. Annunciator Panel ..............................................................................................................CHECK

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

Supplement B-1 Page 9 of 12 4AC

METRO III – ICAO ANNEX 8 SECTION 3A . . . . . . .ABNORMAL PROCEDURES (continued) CRUISE NOTE Reduce EGT 50oC or more before reducing RPM of engine(s) operating with the SRL system inoperative. Set RPM (97% or 100%).

Advance power lever to desired EGT that does not exceed limit EGT per Section 3A of basic manual.

1. Cruise Power ........................................................................... SET (97% RPM, LIMIT EGT MAX) (SEE TABLE, SECTION 3A, BASIC MANUAL) 2. Cabin Pressurization ................................................................................................ AS DESIRED

DESCENT Use procedure in Section 2, basic manual.

NOTE • Determine the torque for the expected surface conditions from the Takeoff Power Check Charts. That torque will provide the initial power setting to be used during balked landing or go-around prior to stabilization of EGT indication(s).

• Determine the maximum allowable SRL INOP EGT for the expected surface conditions (placard or Figure 1). That is the limit EGT to be used on the engine(s) with inoperative SRL during balked landing or go-around.

BEFORE LANDING Use procedure in Section 2, basic manual.

BALKED LANDING NOTE When required for obstacle clearance, this procedure is used to obtain the climb performance depicted in the basic manual.

1. Power Levers ...............................................................................LIMIT EGT OR 100% TORQUE (WHICHEVER OCCURS FIRST)

Supplement B-1 Page 10 of 12 4AC

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

METRO III – ICAO ANNEX 8 SECTION 3A . . . . . . .ABNORMAL PROCEDURES (continued) BALKED LANDING (continued) NOTE Set expected torque from the Takeoff Power Check Charts initially.

Then adjust power lever(s) to SRL INOP EGT limit.

CAUTION TEMPERATURE LIMITER PROTECTION IS NOT AVAILABLE WHEN THE SRL SYSTEM IS INOPERATIVE. SET POWER LEVERS CAREFULLY WHEN ABOVE 50% POWER TO ALLOW FOR EGT INDICATION LAG. IMPROPER POWER MANAGEMENT CAN RESULT IN ENGINE OVER TEMPERATURE CONDITIONS. 2.

3.

4.

5.

6.

7.

8.

9.

Climb Speed ...................................................................................................................... ATTAIN Rate of Climb................................................................ ESTABLISH POSITIVE RATE OF CLIMB Landing Gear............................................................................................................................. UP Flaps .................................................................................................................. RETRACT TO 1/2 Airspeed ........................................................................................... ACCELERATE TO 120 KIAS Flaps .......................................................................................................................................... UP Engine and Propeller Heat Switches ..................................................................... AS REQUIRED Ignition Mode Switches ................................................................... NORMAL OR AS REQUIRED OR Auto/Cont Ignition Switches ................................................................................ AUTO OR CONT

LANDING Use procedure in Section 2, basic manual.

AFTER LANDING Use procedure in Section 2, basic manual.

STOPPING ENGINES Use procedure in Section 2, basic manual.

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90

Supplement B-1 Page 11 of 12 4AC

METRO III – ICAO ANNEX 8 SECTION 4 . . . . . . .PERFORMANCE Determine dry takeoff torque for the takeoff altitude and ambient air temperature plus 5°C. If that expected torque is 100%, read the remaining performance charts at the actual outside air temperature. If the expected torque is less than 100%, use airport ambient air temperature plus 5°C for “OAT” when using the performance charts to determine: • • • • • •

Takeoff torque, The maximum takeoff weight as limited by single engine climb requirements, Accelerate-stop and takeoff distances, Single engine takeoff flight path climb performance, Landing weight as limited by balked landing climb performance, Balked landing rate of climb.

SECTION 5 . . . . . . .WEIGHT AND BALANCE No change.

SECTION 6 . . . . . . .MANUFACTURER’S DATA No change.

Supplement B-1 Page 12 of 12 4AC

SRL OFF/INOPERATIVE FAA Approved: NOV 07/90